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Experimental characterization of the velocity boundary layer in a motored IC engine

机译:电动IC发动机中速度边界层的实验表征

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摘要

The velocity fields near the piston wall are recorded in a motored IC engine during the end of the compression stroke for two different engine speeds and two intake pressure values. Thanks to the use of a Particle Tracking Velocimetry algorithm, the resolution at the wall is sufficient to allow for a study of the boundary layer. The velocity is found to be parallel to the piston with decreasing levels of fluctuations close to the piston surface. Nevertheless these fluctuations are much higher than in canonical boundary layer studies. Even though the values of the momentum-thickness-based Reynolds numbers are extremely low, the boundary layers present shape factors corresponding to turbulent conditions. Using the friction velocity u(tau) to plot the velocity profiles in wall coordinates, a viscous layer can be observed for all cases but a logarithmic region is never found. This is explained by the fact that the friction Reynolds number delta(+) is always too low, meaning that the viscosity-affected near-wall region and the outer region of the boundary layer overlap and prevent the creation of a logarithmic layer. This has strong implications on the use of wall models in numerical simulations. The velocity-defect in the outer region of the boundary layer is shown to scale with delta*/delta u(infinity) rather than with the expected mu(r) from canonical models. These results are attributed to the fact that the turbulence in the core flow in IC engines is not generated by the friction at the wall on the contrary to classical cases. By exchanging momentum with the outer flow, the boundary layer can thus exhibit turbulent properties even though the friction at the wall is rather low.
机译:在压缩冲程结束时,针对两个不同的发动机转速和两个进气压力值,在机动IC发动机中记录了活塞壁附近的速度场。由于使用了粒子跟踪测速算法,墙的分辨率足以进行边界层的研究。发现速度平行于活塞,并且靠近活塞表面的波动水平逐渐降低。然而,这些波动远高于规范边界层研究中的波动。即使基于动量厚度的雷诺数的值非常低,边界层也呈现出与湍流条件相对应的形状因子。使用摩擦速度u(tau)在壁坐标中绘制速度分布图,可以在所有情况下观察到粘性层,但从未找到对数区域。这可以通过以下事实来解释:摩擦雷诺数delta(+)总是太低,这意味着受粘度影响的近壁区域和边界层的外部区域重叠,并阻止了对数层的产生。这对数值模拟中墙模型的使用具有重大影响。边界层外部区域的速度缺陷显示为与delta * / delta u(infinity)成比例,而不是与标准模型的预期mu(r)成比例。这些结果归因于以下事实:与经典情况相反,IC发动机的核心流湍流不是由壁上的摩擦产生的。通过与外部流交换动量,即使壁上的摩擦很小,边界层也可以表现出湍流特性。

著录项

  • 来源
    《International Journal of Heat and Fluid Flow》 |2018年第6期|366-377|共12页
  • 作者单位

    Tech Univ Darmstadt, React Flows & Diagnost, Otto Berndt Str 3, D-64287 Darmstadt, Germany;

    Tech Univ Darmstadt, React Flows & Diagnost, Otto Berndt Str 3, D-64287 Darmstadt, Germany;

    Tech Univ Darmstadt, Inst Fluid Mech & Aerodynam, Alarich Weiss Str 10, D-64287 Darmstadt, Germany;

    Tech Univ Darmstadt, React Flows & Diagnost, Otto Berndt Str 3, D-64287 Darmstadt, Germany;

    Tech Univ Darmstadt, React Flows & Diagnost, Otto Berndt Str 3, D-64287 Darmstadt, Germany;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Ic engine; Boundary layer; Law of the wall; Particle tracking velocimetry;

    机译:内燃机;边界层;壁厚法;颗粒跟踪测速;
  • 入库时间 2022-08-18 02:59:41

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